BS 2A 229-1972 Specification for hexagonal head steel bolts 160000 lbf in2 (1100 MPa)《160 000磅力 平方英寸(1100MPa)六角头钢螺栓规范》.pdf
《BS 2A 229-1972 Specification for hexagonal head steel bolts 160000 lbf in2 (1100 MPa)《160 000磅力 平方英寸(1100MPa)六角头钢螺栓规范》.pdf》由会员分享,可在线阅读,更多相关《BS 2A 229-1972 Specification for hexagonal head steel bolts 160000 lbf in2 (1100 MPa)《160 000磅力 平方英寸(1100MPa)六角头钢螺栓规范》.pdf(16页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD AEROSPACE SERIES BS2A 229:1972 Incorporating Amendment Nos.1,2 and3 Specification for Hexagonal head steel bolts1100MPa UDC 629.7:621.882.211:669.14BS2A229:1972 This BritishStandard, having been approved by the AerospaceIndustry Standards Committee and endorsed by theChairman of the
2、 Engineering Divisional Council, was publishedunder the authority ofthe General Council of theInstitution on 12September1972 BSI02-2000 The following BSI reference relates to the work on this standard: Committee reference ACE/12 Draft for approval 71/35453 ISBN 0 580 07085 9 Amendments issued since
3、publication Amd. No. Date of issue Comments 2129 October1976 2814 April1979 6142 December 1990 Indicated by a sideline in the marginBS2A229:1972 BSI 02-2000 i Contents Page 1 Scope 1 2 General requirement 1 3 Material and manufacture 1 4 Dimensions 1 5 Screw threads 1 6 Anti-corrosion treatment 1 7
4、Identification and marking 1 Appendix A Oversize bolts Inside back cover Appendix B Table for the conversion of inches to millimetre equivalents Inside back cover Figure 1 2 Figure 2 2 Figure 3 3 Figure 4 3 Table 2 Bearing length L and overall length E 3BS2A229:1972 ii BSI 02-2000 This revision of B
5、S A229:1968 has been prepared to incorporate Amendment Slip No.1:1969 (AMD195,) and also to extend the size range to include 9 / 16 18 to1 1 / 4 12 UNJF bolts. Dimensions for oversize bolts are given in Appendix A. It provides a range of1100MPa to1250MPa steel bolts with UNJ profile threads and clos
6、e tolerance shanks for aircraft use. The lengths of the bolts are in fractional increments. This standard requires reference to the following BritishStandards: BS4084, Unified screw threads of “UNJ” basic profile. BSA100, General requirements for bolts and nuts of tensile strength not exceeding1250M
7、Pa. BS S147, Nickel-chromium-molybdenum steel (bar for the manufacture of forged bolts only). BS S148, Low nickel-chromium steel (bar for the manufacture of forged bolts only). BS S149, 1.75per cent nickel-chromium-molybdenum steel. BS S ., 1% chromium-molybdenum steel bars for the manufacture of fo
8、rged bolts and forged nuts 1) . NOTE 1The values in imperial units are to be regarded as the standard. The table in Appendix A provides millimetre equivalents of inch dimensions and is based on the tables in BS350, “Conversion factors and tables”. NOTE 21MPa=1N/mm 2 =1MN/m 2 =145.0lbf/in 2 . Informa
9、tion on SI units is given in BS3763, “The International System of units (SI)”. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself co
10、nfer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, pages1 to10, an inside back cover and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated
11、in the amendment table on the inside front cover. 1) In course of preparation.BS2A229:1972 BSI 02-2000 1 1 Scope This BritishStandard specifies the materials, dimensions, finish and inspection requirements for cadmium plated steel bolts with hexagonal heads and Unified threads for aircraft use. 2 Ge
12、neral requirement The bolts shall be manufactured, inspected and tested in accordance with the requirements of BSA100. 3 Material and manufacture 3.1 The bolts shall be forged from material which complies with the latest issue of one of the following BritishStandards: BS S147 or BS S148 or BS S149 o
13、r BS S . 2) . 3.2 In the finally heat-treated condition, the mechanical properties of the material used for forged bolts shall be as follows: 4 Dimensions 4.1 All bolts, after application of the ant-corrosion coating, shall conform to the dimensions and tolerances given in Table1 and Table 2 or Appe
14、ndix A. 4.2 The run-out of the thread shall comply with the relevant requirements of BS A100. 4.3 The nominal length of the bolt shall be the bearing length L. 4.4 Dimensions of oversize bolts are given in Appendix A. 5 Screw threads The screw threads shall conform to the basic thread form, diameter
15、 and related pitches specified in BS4084, “Unified screw threads of “UNJ” basic profile (Class3A)”. 6 Anti-corrosion treatment All bolts shall be coated with cadmium, in accordance with the relevant requirements of BSA100. 7 Identification and marking The bolts shall be marked on the top face of the
16、 head with the number of this BritishStandard and the relevant part numbers shown in Table 2, e.g.2A229E62. Oversize bolts shall be marked as state in Appendix A. 2) In course of preparation. 0.2% proof stress not less than965MPa Tensile strength not less than1100MPa Elongation on 5.65 S 0 not less
17、than10%BS 2A 229:1972 2 BSI 02-2000 NOTEIt is permissible to suitable chamfer the blank prior to thread rolling operation without any subsequent machining provided dia G and the max. runout of thread at bolt end are maintained. *For bearing length L and overall length E see Table 2 Figure 1 Figure 2
18、 Alternative form of bolt head at the option of the bolt manufacturer Third angle projection 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 Nominal size UNJF Decimal equivalent of nominal size Diameter of plain portion of shank A 2 pitch T min. (reference only) Width across flats B Width across corners C Thick
19、ness of head D Radius under bolt head R Diameter of chamfer G Max. Min. Max. Min. Max. Min. Max. Min. Max. Min. 0.010 in in in in in in in in in in in in in in 1032 0.1900 0.1895 0.1885 .063 0.381 0.376 0.367 0.434 0.419 0.125 0.110 0.025 0.015 0.120 1 / 4 28 0.2500 0.2495 0.2485 .071 0.443 0.439 0.
20、430 0.507 0.491 0.140 0.125 0.025 0.015 0.174 5 / 16 24 0.3125 0.3120 0.3110 .083 0.506 0.502 0.492 0.580 0.561 0.171 0.156 0.025 0.015 0.229 3 / 8 24 0.3750 0.3745 0.3735 .083 0.615 0.564 0.553 0.651 0.631 0.203 0.188 0.025 0.015 0.292 7 / 16 20 0.4375 0.4370 0.4360 .100 0.631 0.690 0.679 0.797 0.7
21、75 0.234 0.219 0.030 0.020 0.344 1 / 2 20 0.5000 0.4995 0.4985 .100 0.757 0.752 0.741 0.868 0.845 0.265 0.250 0.030 0.020 0.406 9 / 16 18 0.5625 0.5615 0.5605 0.111 0.859 0.877 0.865 1.001 0.987 0.296 0.281 0.035 0.020 0.462 5 / 8 18 0.6250 0.6240 0.6230 0.111 0.921 0.940 0.928 1.073 1.059 0.327 0.3
22、12 0.040 0.025 0.524 3 / 4 16 0.7500 0.7490 0.7480 0.125 1.057 1.064 1.052 1.214 1.200 0.390 0.375 0.045 0.030 0.640 7 / 8 14 0.8750 0.8740 0.8730 0.143 1.195 1.252 1.239 1.429 1.414 0.453 0.438 0.050 0.035 0.754 112 1.0000 0.9990 0.9980 0.167 1.314 1.440 1.427 1.643 1.628 0.515 0.500 0.060 0.045 0.
23、865 1 1 / 8 12 1.1250 1.1240 1.1225 0.167 1.463 1.627 1.614 1.856 1.842 0.577 0.562 0.070 0.055 0.990 1 1 / 4 12 1.250 1.2490 1.2475 0.167 1.651 1.814 1.801 2.071 2.055 0.640 0.625 0.075 0.060 1.114BS2A229:1972 BSI 02-2000 3 Table 2 Bearing length L and overall length E NOTEUnallocated part numbers
24、should not be used. Figure 3 Figure 4 No.1032 UNJF 1 / 4 28 UNJF 5 / 16 24 UNJF Part No. L 0.010 E 0.015 Part No. L 0.010 E 0.015 Part No. L 0.010 E 0.015 D2 D3 D4 D5 D6 D7 D8 D9 D10 D11 D12 D13 D14 D15 D16 D17 D18 D19 D20 D21 D22 D23 D24 D25 D26 D27 D28 D29 D30 D31 in 0.125 0.188 0.250 0.312 0.375
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